CA2176052A1 - Transducer having a resonating silicon beam and method for forming same - Google Patents

Transducer having a resonating silicon beam and method for forming same

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Publication number
CA2176052A1
CA2176052A1 CA002176052A CA2176052A CA2176052A1 CA 2176052 A1 CA2176052 A1 CA 2176052A1 CA 002176052 A CA002176052 A CA 002176052A CA 2176052 A CA2176052 A CA 2176052A CA 2176052 A1 CA2176052 A1 CA 2176052A1
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CA
Canada
Prior art keywords
type
layer
cavity
dopant
substrate
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
CA002176052A
Other languages
French (fr)
Inventor
James D. Seefeldt
Michael F. Mattes
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SSI Technologies LLC
Original Assignee
SSI Technologies LLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by SSI Technologies LLC filed Critical SSI Technologies LLC
Publication of CA2176052A1 publication Critical patent/CA2176052A1/en
Abandoned legal-status Critical Current

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Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P15/00Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
    • G01P15/02Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
    • G01P15/08Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values
    • G01P15/0802Details
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L1/00Measuring force or stress, in general
    • G01L1/18Measuring force or stress, in general using properties of piezo-resistive materials, i.e. materials of which the ohmic resistance varies according to changes in magnitude or direction of force applied to the material
    • G01L1/183Measuring force or stress, in general using properties of piezo-resistive materials, i.e. materials of which the ohmic resistance varies according to changes in magnitude or direction of force applied to the material by measuring variations of frequency of vibrating piezo-resistive material
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L9/00Measuring steady of quasi-steady pressure of fluid or fluent solid material by electric or magnetic pressure-sensitive elements; Transmitting or indicating the displacement of mechanical pressure-sensitive elements, used to measure the steady or quasi-steady pressure of a fluid or fluent solid material, by electric or magnetic means
    • G01L9/0001Transmitting or indicating the displacement of elastically deformable gauges by electric, electro-mechanical, magnetic or electro-magnetic means
    • G01L9/0008Transmitting or indicating the displacement of elastically deformable gauges by electric, electro-mechanical, magnetic or electro-magnetic means using vibrations
    • G01L9/0019Transmitting or indicating the displacement of elastically deformable gauges by electric, electro-mechanical, magnetic or electro-magnetic means using vibrations of a semiconductive element
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L9/00Measuring steady of quasi-steady pressure of fluid or fluent solid material by electric or magnetic pressure-sensitive elements; Transmitting or indicating the displacement of mechanical pressure-sensitive elements, used to measure the steady or quasi-steady pressure of a fluid or fluent solid material, by electric or magnetic means
    • G01L9/0041Transmitting or indicating the displacement of flexible diaphragms
    • G01L9/0042Constructional details associated with semiconductive diaphragm sensors, e.g. etching, or constructional details of non-semiconductive diaphragms
    • G01L9/0045Diaphragm associated with a buried cavity

Abstract

A method of forming apparatus including a force transducer on a silicon substrate having an upper surface, the silicon substrate including a dopant of one of the n-type or the p-type, the force transducer including a cavity having spaced end walls and a beam supported in the cavity, the beam extending between the end walls of the cavity, the method including the steps of: (a) implanting in the substrate a layer of a dopant of said one of the n-type or the p-type; (b) depositing an epitaxial layer on the upper surface of the substrate, the epitaxial layer including a dopant of the other of the n-type or the p-type; (c) implanting a pair of spaced sinkers through the epitaxial layer and into electrical connection with said layer, each of the sinkers including a dopant of the one of the n-type or the p-type; (d) anodizing the substrate to form porous silicon of the sinkers and the layer; (e) oxidizing the porous silicon to form silicon dioxide; and (f) etching the silicon dioxide to form the cavity and beam.

Description

2i 76052 TRANSDUCER HAVING A RESONATING SILICON BEAM
AND METHOD FOR FORMING SAME
BAQICGROUND OF THE INVENTIQN
Field of the Invention The invention relates to apparatus such as pressure sensors which include a force transducer having a resonating silicon beam formed in a silicon wafer, and particularly to a method for forming the same.
Discussion of Prior Art U.S. Pat. No. 5,090,254 to Guckel discloses a polysilicon resonating beam transducer. The transducer includes a beam of polysilicon which is mounted at its ends in a silicon substrate or wafer. The substrate and a polysilicon shell cooperate to define a cavity around the beam. The cavity is sealed from the atmosphere and evacuated to maximize the Q of the resonating beam. Resonant excitation of the beam can be accomplished in various ways, such as by capacitive excitation. Vibratory motion of the beam may be detected using an implanted resistor which is piezoresistive. Formation of the beam is carried out by depositing the beam on a sacrificial layer and surrounding the beam in a second sacrificial layer before the encapsulating polysilicon shell is formed.
The sacrificial layers are etched out with liquid etchant which passes through channels in the periphery of the shell. Following etching, the interior of the cavity surrounding the beam is maintained in a wash liquid so that the beam is not deflected toward any of the adjacent surfaces, and the wash liquid is removed by freezing and sublimation. The interior surfaces of _ the cavity and the outer surfaces of the beam are passivated, and the channels leading into the cavity are sealed by oxidation in an oxidizing atmosphere, which also results in consumption of oxygen in the cavity.
U.S. Pat. No. 5,242,863 to Xiang-Zheng et al.
relates to a silicon diaphragm piezoresistive pressure sensor having a diaphragm formed by a single-sided fabrication method. The diaphragm is formed with a cavity thereunder by: a) forming a buried low resistance layer under a predetermined diaphragm region; b) epitaxially depositing a layer of silicon;
c) forming low resistance trenches through the epitaxial layer which trenches are connected with the buried low resistance layer at the edge of the buried low resistance layer; d) converting the low resistance trenches and buried low resistance layer to porous silicon by anodization in a concentrated HF solution;
e) removing the porous silicon by etching; and f) filling the openings formed by etching with polysilicon to seal the cavity.
SCARY OF THE INVENTION
The invention provides apparatus including a force transducer having a resonating beam that is formed in a silicon wafer and which apparatus is of relatively simple and inexpensive construction. As used herein, the term beam should be interpreted broadly to include microstructures such as tuning forks, H-beams, cross beams, interleaved combs, and spiral springs, etc.
The invention also provides a method having relatively few manufacturing steps for forming apparatus including a force transducer having a resonating beam formed in a silicon wafer. In one form, the method includes the steps of implanting in a substrate a layer of either n-type or the p-type dopant; depositing a doped epitaxial layer on the upper surface of the substrate (wherein the dopant in the epitaxial layer i.s the opposite from that type of dopant in the substrate, i.e., if the substrate has therein a p-type dopant, then the epitaxial layer includes an n-type dopant and vice versa); implanting a pair of spaced sinkers through the epitaxial layer and into electrical connection with the epitaxial layer, each of the sinkers including either the n-type or p-type dopant; anodizing the substrate to form porous silicon from the sinkers and the underlying doped substrate layer; oxidizing the porous silicon to form silicon dioxide; and etching the silicon dioxide to form the cavity and beam..
It is an advantage of the invention to provide a method of forming a single crystal resonating beam within a cavity, which beam facilitates the placement: of electronic circuitry directly on the beam.
According too one aspect of the invention, there is provided a methcd of forming apparatus including a force transducer hav_Lng a resonating silicon beam within a cavity in a silicon substrate, the method comprising the acts of:
a. providina-t~he silicon substrate having an upper surface;
b. implanting a buried layer of a dopant, the dopant being one of the n-type and the p-type dopant,. in the substrate;
c. implanting in the substrate a layer of a dopant of the other of the n-type and the p-type over the buried layer of the one of the n-type and the p-type dopant,;
d. depositing ar. epitaxial layer on the upper surface of: the sub~~t:rate to completely cover the layer of dopant, the epitaxi.a:1 layer including a dopant of the one of the n-type and the p-type;
e. implanting a pair of spaced sinkers through the epitaxial layer and into electrical connection with l~he layer of c~opant, eacz of the sinkers including a dopant of the other of the :~-type and the p-type;
f. anodizinc3 the substrate to form porous silicon of the sinkers and t:he layer of dopant;
g. oxidizing the porous silicon to form silicon dioxide;

- 4a -h. dissolving the silicon dioxide by etching to form the cavity and t:he beam supported within the cavity to resonate within the cavity, so that the cavity includes a pair of spaced side walls, a pair of spaced end walls extending between the side walls, and a bottom wall, and so that the beam extends from one of the end walls of the cavity to the other of the end walls of the cavity, and so that t:he beam has side surfaces spaced from the side walls of the cavity and a lower surface spaced from the bottom wall; and i. providing a capacitive drive for causing resonant motion of the beam, the capacitive drive including a first electrode below the beam, a second electrode in the bears, and a third electrode above the beam wherein the buried layer of the one of the n-type and the p-type dopant~ acts as the first electrode.
According t;o another aspect of the invention, there is provided a rnethod of forming apparatus including a force transducer having a resonating silicon beam within a cavity in a silicon substrate, the method comprising the acts of:
a. providing the silicon substrate having an upper surf ace ;
b. implanting a buried layer of a dopant, the dopant being one of the n-type and the p-type dopant, in the substrate;
c. implanting in the substrate a layer of. a dopant of the other' of the n-type and the p-type over the buried layer of the one of the n-type and the p-type dopant;
d. depositing an epitaxial layer on the upper surface of the subw~t:rate to completely cover the - 4b --layer of dopant, the epitaxial layer including a dopant of the one of the n-type and the p-type.
e. implanting a pair of spaced sinkers through the epitaxial. layer and into electrical connection with the layer of dopant, each of the sinkers including a dopant of t:he other of the n-type and the p-type.
f. anodi~:ing the substrate to form porous silicon of the sinkers and the layer of dopant;
g. oxid:i~:in~~ the porous silicon to form silicon dioxide;
h. form:inc~ a sacrificial layer over the epitaxial layer;
i. form:ing over the sacrificial layer a cover layer;
j. dissol.vi:ng the silicon dioxide and the sacrificial layer by etching to form the cavity and the beam supported within the cavity to resonate within the cavity, so that the cavity includes a pair of spaced side walls, a pair of spaced end walls extending between the side walls, a bottom wall, and a top wall, and so that the beam extends from o:ne of the end walls of the cavity to the other of the end walls of the cavity, and so that the beam has side surf=aces spaced from the side wall's of the cavity, a lower ~~urface spaced from the bottom wall and an upper surface spaced from the top wall;
k. prov:ic~ing a capacitive drive for causing resonant motion of the :beam, the capacitive drive including a first electrode and wherein the buried layer of the one of the n-type and the p-type dopant acts as the first electrode of the capacitive drive.
According t:o a further aspect of the invention, - 4c _ there is provided a rnethod of forming apparatus including a force transducer having a single crystal resonating silicon beam within. a cavity in a single crystal silicon substrate, the method comprising the acts of:
a. providing the single crystal silicon substrate having an. upper surface;
b. implanting a buried layer of a dopant, the dopant being one of the n-type and the p-type dopant, in the substrate;
c. implanting in the single crystal substrate a layer of a dopant of the other of the n-type and the p-type over the buried layer;
d. depositing an epitaxial layer on the upper surface of the single crystal substrate to completely cover the layer of dopant, the epitaxial layer including a dopant of the one of the n-type and the p-type;
e. implanting a pair of spaced sinkers through the epitaxial layer and into electrical connection. with the .Layer of dopant, each of the sinkers including a dopant of the other of the n-type and the p-type;
f. anodi~:ing the substrate to form porou:~
silicon of the sinkers and the layer of dopant;
g. oxidising the porous silicon to form silicon dioxide;
h. dissolving the silicon dioxide by etching to form tr.e cavity and the single crystal silicon beam supported within the cavity to resonate within the cavity, sc~ that the cavity includes a pair of spaced side walls, a pair of spaced. end walls extending between the side walls, and a bottom wall, and so that the beam extends from one of i~ize end walls of the cavity to the - 4d -other of the end walls of the cavity, and so that the beam has side surfaces spaced from the side walls of the cavity and. a lower surface spaced from the bottom wall;
and i. providing a capacitive drive for causing resonant motion of the beam, the capacitive drive including a first elc=_ctrode below the single crystal silicon beam, a second electrode in the beam, and a third electrode above the beam and wherein the buried layer acts as tile first ele~trode.
Other features and advantages of the invent=ion will become apparent to those skilled in the art upon review of the following detailed description, claims, and drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
Fig. 1 i~~ a cross-sectional view of a force transducer die embodying various of the features of the invention and taken along line 1-1 of Fig. 26.
Fig. 1A i.s a cross-sectional view of a forage transducer die taken along line lA-lA in Fig. 1.
Fig. 2 i:~ a cross-sectional view similar to Fig. 1 and showing a buried n-type layer implanted i:n the substrate.
Fig. 3 i;~ a buried n--type layer mask used in the process of creating the buried n-type layer shown in Fig. 2.
Fig. 4 i;~ a view similar to Fig. 2 and showing a buried p-type layer.
Fig. 5 i:~ a buried p-type layer mask for patterning the buried p-type layer shown in Fig. 4.
Fig. 6 is a view similar to Fig. 4 and showing an n-type epitaxial layer and two p-type sinkers.
Fig 7. is a p-type sinker mask for patterning the p-type sinkers shown in Fig. 6.
Fig. 8 is a view similar to Fig. 6 and showing an n-type sinker.
Fig. 9 is an-n-type sinker mask for patterning the n-type sinker shown in Fig. 8.
Fig. 10 is a view similar to Fig. 8 and showing a precavity region.
Fig. 11 is a view similar to Fig. 10 and showing p-type layers defining a capacitor middle layer and piezoresistor.
Fig. 12 is a capacitor and piezoresistor mask for patterning the p-type layers defining the capacitor middle layer and piezoresistor shown in Fig. 1I.
Fig. 13 is a view similar to Fig. 11 and showing a sacrificial layer.
Fig. 14 is a sacrificial layer mask for patterning the sacrificial layer shown in Fig. 13. -Fig. 15 is a view similar to Fig. 13 and showing a cover layer and anchors.
Fig. 16 is an anchor mask for patterning the anchor cavities shown in Fig. 15.
Fig. 17 is a cover mask for patterning the cover layer shown in Fig. 15.
Fig. 18 is a view similar to Fig. 15 and showing an upper p-type layer implanted in the cover layer.
Fig. 19 is an upper p-type layer mask for patterning the upper p-type layer shown in Fig. 18.
Fig. 2O is a view similar to Fig. 19 and showing a cavity and open etch channels.
Fig. 21 is a view similar to Fig. 20 and showing the sealed etch channels and an insulating layer.
Fig. 22 is a view similar to Fig. 21 and showing electrical contact cavities.
Fig. 23 is an electrical contact mask for patterning the electrical contact cavities shown in Fig. 22.
Fig. 24 is a view similar to Fig. 22 and showing metal electrical contacts.
Fig. 25 is a metal mask for patterning the metal electrical contacts shown in Fig. 24.
Fig. 26 is an illustration showing a force transducer of the invention.
Before one embodiment of the invention is explained in detail, it is to be understood that the invention is not limited in its application to the details of the construction and the arrangements of components set forth in the following description or illustrated in the drawings. The invention is capable of other embodiments and of being practiced or being ~~ ~~fl~2 carried out in various ways. Also, it is to be understood that the phraseology and terminology used herein is for the purpose of description and should not -be regarded as limiting.
DETAILED DESCRIPTION OF A PREFERRED EMBODIMENT
Illustrated in the drawings is an apparatus 4 formed on a silicon wafer or substrate 8 and embodying various of the features of the invention. Although different apparatus such as pressure sensors, strain sensors and displacement sensors may be formed according to the invention, in the illustrated embodiment the apparatus 4 is a force transducer 10.
The force transducer 10 (Fig. 26) includes a resonating beam formed as further described below.
The force transducer 10 also includes integrated circuitry 12 formed on the substrate 8 and connected to the force transducer 10. The integrated circuitry 12 provides power for the force transducer 10 and converts output from the force transducer 10 to a desired format. It will be appreciated by those skilled in the art that the integrated circuitry 12 can be suitably arranged in various configurations. The configurations of the integrated circuitry 12 are known and will not be described in further detail.
As shown specifically in Figs. 1 and 2, the wafer or substrate 8 is a single crystal of silicon which is altered as described below. The wafer 8 ~176~52 _g_ includes spaced upper and lower side portions 16 (Fig. 2, lower side portion not shown). The upper side portion 16 includes a horizontal upper surface 17.
Although the wafer 8 can be of any suitable thickness, in the illustrated embodiment the wafer 8 is about 500 microns thick. An epitaxial layer is deposited on the upper surface 17, as further described below.
A cavity 22 is defined in the upper side portion 16. For purposes of describing the cavity 22, the upper side portion 16 of the wafer 8 is taken to include the epitaxial layer (i.e., as shown in the drawings, portions of the cavity 22 are defined by the epitaxial layer deposited on the upper surface 17).
The cavity 22 includes a pair of spaced side walls 28, a pair of spaced end walls 32 extending between the side walls 28, and a horizontal bottom wall 36 extending between the side walls 28 and end walls 32.
The side walls 28, end walls 32 and bottom wall 36 thus cooperate to define the cavity 22.
The transducer 10 includes a beam 52 which is supported in the cavity 22. The beam 52 has a longitudinal axis and includes opposite end portions 56 (shown only in Fig. 1A) spaced along the longitudinal axis. The end portions 56 are connected to and integral with the end walls 32. The beam 52 being thus supported can be described as an end-supported or doubly-supported beam. Attachment of the beam 52 at the end portions 56 allows strains in the wafer 8 in 2176~~2 _g_ the direction of the longitudinal axis of the beam 52 to cause changes in the resonant frequency of the beam 56. in the specific embodiment illustrated, the beam 52 is formed in the epitaxial layer 208 (Figs. 8 and 10). In other specific embodiments (not shown), the beam 52 can be formed partially in the epitaxial layer 208 and in the upper side portion 16 of the wafer 8.
The beam 52 has a length defined between the end walls 32. Although the beam 52 can be of any suitable length, in the illustrated embodiment the length of the beam 52 is about 100 um. The beam 52 includes a lower side 64 spaced from the bottom wall 36. The beam 52 also includes an upper side 68 spaced from the lower side 64. The beam 52 has a thickness between the lower and upper sides 64 and 68. Although the beam can be of any suitable thickness, in the illustrated embodiment the beam 52 has a thickness of about 1.5 microns. The beam 52 also includes a pair of spaced sides 72 extending between the lower and upper sides 64 and 68 parallel to the side walls 28. The beam 52 has a width defined between the sides 72, which in the illustrated embodiment is about 20 microns.
The transducer 10 includes a cover layer 92 (Fig. 15) spaced from the upper side 68 of the beam 52.
The cover layer 92 is supported about its periphery by the epitaxial layer 208 around the cavity 22. The cover layer 92 cooperates with the side walls 28, end walls 32 and bottom wall 36 to enclose the cavity 22 ~

2i ~6ii52 and thus define a closed space about the beam 52.
Although any suitable material is appropriate, in the illustrated embodiment, the cover layer 92 consists of polysilicon having a thickness of about 2 microns.
Although the space between the cover layer 92 and the upper side portion 68 of the beam 52 can be of any suitable dimension, in the illustrated embodiment the cover layer 92 is spaced about 1 micron above the upper -side 68 of the beam 52. Preferably, the cavity 22 is evacuated to minimize damping of the vibrations of the beam, as further described below.
The transducer 10 includes means 120 (Fig.
26) for causing resonant motion of the beam. Although any suitable means can be employed for causing resonant motion of the beam, in the illustrated embodiment the means 120 for causing resonant motion of the beam 52 comprises electrodes which cooperate to define a capacitive drive 120. The capacitive drive 120 includes spaced lower, middle and upper electrodes or conductive regions 200, 224a, and 229 (shown in Fig.
20). The lower conductive region 200 is an n-type dopant, such as phosphorous, implanted in the substrate 8 below the bottom wall 36. The middle conductive region 224a is a p-type dopant, such as boron, implanted in the beam 52. The upper conductive region 229 is a p-type dopant, such as boron, implanted in a polysilicon cover, as described below. The lower, middle and upper conductive regions 200, 224a and 229 ~

are electrically connected to the integrated circuitry 12 to define a capacitor or capacitive drive. It will be apparent to those skilled in the art that the beam 52 is caused to vibrate or resonate by operation of the capacitive drive in a known manner. It is also apparent that various combinations of dopants can be used to form the electrodes 200, 224a and 229.
The transducer IO includes means 124 (Fig.
26) for measuring resonating motion of the beam 52.
Although any suitable means can be used for measuring resonating motion of the beam, in the illustrated embodiment the means 124 for measuring resonating motion of the beam is a piezoresistor. The piezoresistor 124 is created by implanting in the beam 52, a dopant, such as boron. The piezoresistor 124 is connected to the integrated circuitry 12 in manner well known to those of ordinary skill in the art. The resistance of the piezoresistor 124 changes with strain in the beam 52 in accordance with the piezoresfstive effect, and thus permits resonance of the beam to be measured in a known manner. It will be appreciated by those skilled in the art that in different embodiments (not shown) other specific arrangements of passive electronic circuit elements such as a capacitor or arrangement of active electronic circuitry can be used for measuring the resonant frequency of the beam.
Moreover, the single crystal nature of the beam 52 allows the placement of active or passive signal 2i 7652 conditioning circuitry (not shown) to be implanted directly on the beam 52.
The transducer 10 includes electrical contacts 130, 131 and 134 for connecting the capacitive drive 120 and piezoresistor 124 to the integrated circuitry 12. In the illustrated embodiment, the electrical contacts 130, 131 and 134 comprise conductive material, such as aluminum, which is deposited on the epitaxial layer 208. In other embodiments (not shown), the electrical contacts may be formed by dopants implanted to define conductive regions .
The transducer 10 is formed on any suitable silicon wafer or substrate 8. A suitable substrate 8 is a p-type silicon wafer of lightly doped P{100) silicon having p-type boron dopant with a carrier concentration between 1015 and lOlfi cm3, a <100> cut lattice, 6.0-18.0 ohm-cm resistance. Wafers meeting SEMI standard prime CZ or float zone, for example, are suitable. Examples of other suitable silicon wafers are those having lower concentrations of p-type or n-type dopants than layers to be subsequently added to the wafer, such that the dopant acts as an etch stop at the boundary with the added layers.
The beam 52 having the specific construction described herein is formed by altering the p-type wafer 8 according to the following steps:

217b052 1. implanting buried n-type layer 200 in the p-type wafer 8;
2. implanting buried p-type layer 204 over the buried n-type layer 200;
3. depositing an epitaxial n-type layer 208 on the upper surface 17 of the wafer 8;
4. implanting p-type sinkers 212 and 216 through the epitaxial n-type layer 208 and into connection with the p-type layer 204;
5. implanting an n-type sinker 220 through the epitaxial n-type layer 208 and into electrical connection with the n-type layer 200;
6. forming porous silicon of the p-type layer 204 and the p-type sinkers 212 and 216 by anodization;
7. oxidizing the porous silicon to form silicon dioxide in a pre-cavity region;
8. implanting p-type layers 224, 225 and 226 in the epitaxial n-type layer 208;
9. depositing a sacrificial layer 228;
10. etching the sacrificial layer 228;
11. growing anchor oxide 227;
12. forming anchor cavities 231 by etching anchor oxide 227;
13. depositing the cover layer 92;
14. implanting p-type layer 229 in the cover layer 92;
15. etching the cover layer 92;
16. dissolving the sacrificial layer 228 and the porous silicon dioxide by etching to form the cavity 22;
17. sealing and evacuating the cavity 22;
18. depositing an insulating layer 234;
19. etching contact cavities 235 through the insulating layer 234; and 20. depositing electrical contacts 232 for connection to the integrated circuitry 12.
It will be appreciated by those skilled in the art that various of the above-mentioned steps may be omitted or altered in different specific embodiments of the invention. For example, the steps regarding the n-type layer 200, the n-type sinker 220 and the p-type layers 224 and 226 may differ if different means are employed for causing resonance of the beam or for measuring the resonant frequency of the beam.
In the illustrated embodiment, the wafer 8 is prepared for implantation of the buried n-type layer ZO 200 by initially forming a screening layer of Si02 on the upper surface 17 of the wafer 8. In the illustrated embodiment, the screening layer of SiOz has a thickness of about 5000 +/- 500 angstroms. The Si02 can be formed by any suitable means. In the illustrated embodiment, oxidation to form the SiOz screening layer is carried out by first "pushing" with about 2.25 liters per minute (1/m) of NZ at a temperature of about 550°C for a period of about 4 217b052 hours, ramping about 2.25 1/m of OZ gas at a rate of _._. _ about 20°C/minute, oxidizing with about 2.25 1/m of HZ
and OZ at about 1000°C, and then ramping with about 8 1/m of NZ at a rate of about 20°C/minute. The term "pushing" as used herein means inserting the wafer into the furnace. As also used herein, the term "ramping"
means changing the temperature in the furnace. The SiOz screening layer is thereafter etched to achieve a substantially uniform thickness. Etching with a 10:1 buffered oxide etching solution for a period of about 5 minutes is suitable. A suitable etching solution includes about 40~ ammonia fluoride, 15?c hydrogen fluoride and 45$ water. Those skilled in the art will recognize that forming and etching a screening layer of SiOz before each implant or deposition step may assist in control of the subsequent implantation or deposition step. In other embodiments, any of the screening layers of Si02 may be omitted.
The buried n-type layer 200 can be implanted by any suitable means. In the illustrated embodiment, the buried n-type layer 200 (Fig. 2) is patterned by applying photoresist and then exposing the photoresist with the buried n-type layer mask shown in Fig. 3, removing the mask, and then dosing with a suitable n-type dopant. In the illustrated embodiment, the n-type dopant is phosphorous, which is dosed at a concentration of 5 x 10" cm 2 at 150 KeV. After the photoresist is removed, the buried n-type layer 200 is 2i7b052 driven to a final thickness of about 3 microns by thermal annealing. Thermal annealing can be carried out in any suitable manner, such as by pushing with 2.25 1/m of NZ at 850°C for a period of about 30 minutes, ramping 2.25 1/m of 02 at a rate of 20°C/minute, oxidizing with 2.25 1/m of NZ at about 1050°C for a period of about 2 hours, and ramping with 8 1/m of NZ at a rate of 20°C/minute. The thermal annealing conditions specifically described above are provided for illustration, and those skilled in the art will appreciate that different conditions may be used to achieve this result.
The buried p-type layer 204 (Fig. 4) is implanted over the buried n-type layer 200 by any suitable means. In the illustrated embodiment, the wafer 8 is prepared for receiving the p-type layer 204 by first etching for 5 minutes to remove the Si02 formed in the previous thermal annealing step. The buried p-type layer 204 is patterned by applying photoresist and exposing the photoresist with the mask shown in Fig. 5. In the illustrated embodiment, the p-type dopant is boron. The boron is dosed at a concentration of 5 x 1013 cm z at energy levels of 50, 100 and 150 lZeV. After the buried p-type layer 204 is implanted and the photoresist is removed, the buried p-type layer 204 is driven by thermal annealing to a final thickness of about 1 Vim. Thermal annealing can be carried out by pushing with 2.25 1/m of OZ at 850°C

2~76u52 for a period of about 30 minutes, ramping 2.25 1/m of OZ at a rate of 20°C/minute, annealing with 2.25 1/m of N2 at about 1000°C for a period of about 10.5 hours, and ramping with 8 1/m of NZ at a rate of 20°C/minute.
The n-type epitaxial layer 208 (Fig. 6) is deposited on the entire upper surface 17 of the wafer 8 by epitaxial deposition. In the illustrated embodiment, the wafer 8 is prepared for receiving the n-type epitaxial layer 208 by etching to remove the Si02 formed in the previous thermal annealing step.
The n-type epitaxial layer 208 is deposited in a conventional manner. In the illustrated embodiment, the n-type epitaxial layer 208 has a thickness of about 2 +/- 0.2 microns and a resistivity of about 0.35 +/-0.05 ohms-cm.
The p-type sinkers 212 and 216 (Fig. 6) are implanted in the n-type epitaxial layer 208 and into electrical connection with the p-type layer 204. In the illustrated embodiment, the n-type epitaxial layer 208 is prepared for receiving the p-type sinkers 212 and 216 by partially oxidizing the n-type epitaxial layer 208 to form a screening layer of SiOz having a thickness of about 500 +/- 50 angstroms. The Si02 can be formed by first "pushing" with about 2.25 liters per minute (1/m) of Hzand Oa at a temperature of about 850°C for a period of about 10 minutes, and then oxidizing with about 2.25 1/m of HZ and OZ at about 850°C for a period of about 30 minutes. The p-type sinkers 212 and 216 are patterned by applying photoresist and exposing the photoresist with the mask shown in Fig. 7. In the illustrated embodiment, the p-type dopant is boron dosed at a concentration of 5 x 1013 cm'Z at an energy level of 120 KeV. After the p-type sinkers 212 and 216 are implanted, the photoresist is removed.
The n-type sinker 220 (Fig. 8) is implanted through the n-type epitaxial layer 208 and into electrical connection with the n-type layer 200. The n-type sinker 220 is patterned by applying photoresist and exposing the photoresist with the mask shown in Fig. 9. Fig. 2 specifically shows the n-type buried layer mask 219 in phantom, the poly cover layer mask 221 in phantom and the n-sinker mask 222. In the illustrated embodiment, the n-type dopant is phosphorous dosed at a concentration of 5 x 1015 cm'z at an energy level of 80 KeV. After the n-type sinker 220 is implanted and the photoresist is removed, the p-type sinkers 212 and 216 and the n-type sinker 220 are driven to final thickness by thermal annealing.
Thermal annealing can be carried out in any suitable manner, such as by pushing with 2.25 1/m of NZ at 850°C, ramping with 2.25 1/m of 02 at a rate of ZO°C/minute, annealing with 2.25 1/m of NZ at about 1000°C for a period of about 10 hours, and ramping with 8 1/m of NZ at a rate of 20°C/minute to 850°C. The p-type sinkers 212 and 216 thus are driven into electrical connection with the p-type layer 204, and the n-type sinker 220 thus is driven into electrical connection with the buried n-type layer 200.
The p-type layer 204 and the p-type sinkers 212 and 216 are anodized to form a pre-cavity region 223 (Fig. 10) consisting of porous silicon. Those skilled in the art will appreciate that anodization of the p-type layer 204 and the p-type sinkers 212 and 216 is an electrochemical process which can be carried out in any suitable manner. In the illustrated embodiment, anodization is carried out in an electrochemical cell containing from 10 to 50 weight percent hydrofluoric acid. The electrochemical cell is separated into two chambers by the wafer 8 being anodized. Two platinum plates serve as the anodic and cathodic electrodes.
The back or lower side portion of the wafer 8 faces the anodic electrode and the upper side portion 16 faces the cathodic electrode. An anodization voltage between about 1 and 7 volts is applied across the electrodes.
The anodization process automatically stops when the low resistance p-type layer 204 and p-type sinkers 212 and 216 are converted into porous silicon. The porous silicon thus defines a pre-cavity region 223 in the area previously occupfed by the p-type layer 204 and p-type sinkers 212 and 216.
The porous silicon in the pre-cavity region 223 is oxidized to form silicon dioxide. The porous silicon can be oxidized in any suitable manner. In the illustrated embodiment, the porous silicon is oxidized by first "pushing" with about 2.25 liters per minute (1/m) of Oa at a temperature of about 300°C for a period of about 1 hour to stabilize the porous silicon, ramping with 2.25 1/m of OZ at 20°C/minute, and oxidizing with 2.25 1/m of Hz and OZ at 850°C for about 30 minutes to 1 hour, such that the oxide thickness is between about 1000-3000 angstroms. In the illustrated embodiment, the maximum oxidation temperature is maintained at 850°C in order to avoid inelastic change in the resulting oxide. Upon oxidation, the porous silicon in the pre-cavity region is converted to silicon dioxide, and a layer of silicon dioxide having a thickness of about 1500 angstroms is incidentally formed over the entire upper surface of the n-type epitaxial layer 208.
The p-type layer 224 (Fig. 11) is implanted in the n-type epitaxial layer 208 by suitable means.
The p-type layer 224 is patterned by applying photoresist and exposing the photoresist with the mask shown in Fig. 12. In the illustrated embodiment, the p-type dopant is boron dosed at a concentration of 5 x 1015 cm 2 at an energy level of 80 ReV. After the p-type layer 224 is implanted and the photoresist is removed, the p-type layer 224 is annealed. In the illustrated embodiment, the p-type layer 224 is annealed by pushing with 2.25 1/m of NZ at 850°C for a period of 10 minutes and oxidizing with 2.25 1/m of NZ

1 2i?6G52 at 850°C for 30 minutes. The p-type layer 224 defines the middle conductive region 224a of the capacitive drive 120. A second portion 224b of the p-type layer 224 defines an electrical pathway communicating with the upper conductive region 229 of the capacitive drive 120 and with an electrical contact, as further described below. A third portion (not shown in cross section) of the p-type layer 224 defines the piezoresistor 124. The piezoresistor 124 is identified in the mask shown in Fig. 12 as the portion having two legs.
A Layer of sacrificial material is deposited over the entire n-type epitaxial layer 208 and precavity region 223 and then etched to define the sacrificial layer 228 (Fig. 13). In the illustrated embodiment, the sacrificial material is deposited over the n-type epitaxial layer 208. The sacrificial material is a low temperature oxide glass (LTO glass) having a thickness of about 1 micron. The LTO glass is deposited in a known manner, such as by chemical vapor deposition (CVD). In other embodiments, the sacrificial layer can be silicon nitride or another suitable material. The LTO glass is patterned by applying photoresist and exposing the photoresist with the mask shown in Fig. 14. The LTO glass is etched and the mask is removed to leave the sacrificial layer 228 (Fig. 13). Etching with a 10:1 buffered oxide etching solution for a period of about 10 minutes is suitable i 2176052 to form the sacrificial layer 228. The photoresist thereafter is removed.
The wafer 8 is prepared for receiving the cover layer 92 by forming anchor cavities 229 in a layer of anchor oxide 227 (Fig. 15). In the illustrated embodiment, the anchor cavities 229 are formed in a layer of SiOZ. A suitable layer of Si02 having a thickness of about 1500 angstroms can be formed by oxidized with 2.25 1/m of HZ and OZ at 850°C
for a period of 30 minutes. The anchor cavities 229 are patterned by applying photoresist and exposing the photoresist using the anchor mask shown in Fig. 16.
The wafer is etched to form the anchor cavities 229 (Fig. 15) in the layer of SiOz. Etching with a 10:1 buffered oxide etching solution for a period of about 1.5 minutes is suitable to form the anchor cavities 229. The photoresist thereafter is removed.
A layer of cover material is deposited over the entire upper side portion of the wafer and then etched to define the cover layer 92 (Fig. 17). Any suitable cover material can be used. In the illustrated embodiment; the cover material is polysilicon deposited on the wafer by low pressure chemical vapor deposition (LPCVD). The polysilicon is suitably deposited at a temperature of about 580°C to about 650°C to a thickness of about 1 to 2 microns.
The polysilicon thus deposited is firmly secured to the wafer by polysilicon which fills the anchor cavities -a3-229 and thus defines integral polysilicon anchors. The cover layer (Fig. 17) is patterned by applying photoresist and exposing the photoresist using the cover mask shown in Fig. 17. The polysilicon is etched to form the cover layer 92. Any suitable polysilicon etching technique can be used. For example, plasma etching with SF6 is suitable to form the cover layer 92. The photoresist thereafter is removed.
The p-type layer 229 (Fig. 18) is implanted in the polysilicon cover layer 92 in a suitable manner.
The p-type layer 229 is patterned by applying photoresist and exposing the photoresist with the. mask shown in Fiq. I9. In the illustrated embodiment, the p-type dopant is boron dosed at a concentration of between 5 x 101° cm'z and 5 x lOls ciaz at an energy level of 60-160 ReV. After the p-type layer 229 is implanted, the photoresist is removed.
The porous silicon dioxide in the precavity region 223 is removed or dissolved by etching to form the cavity 22 (Fig. 20). Any suitable etchant may be employed. In the illustrated embodiment, the etchant is hydrofluoric acid vapor. The use of hydrofluoric acid vapor to etch the cavity 22 avoids having to later dry the cavity. In other embodiments, such as when a liquid etchant is used, it may be necessary to rinse the cavity with water and to dry the cavity by a technique such as sublimation of cyclohexane, as is known in the art. The hydrofluoric acid vapor etches away the SiOz between the anchors 229, thus forming open etch channels 233 in the layer underneath the cover layer 92, and thereafter etches away the LTO
glass forming the sacrificial layer 228 and the silicon dioxide in the precavity region 223. The cavity 22 thus formed is open, in the sense that the etch channels 233 (Fig. 20) were formed by etching in the spaces between the anchors 229 and underneath the cover layer 92.
The cavity 22 is sealed and evacuated in a suitable manner. It is preferred to evacuate the cavity in order to maximize Q of the resonating beam.
In the illustrated embodiment, the wafer is oxidized to form residual SiOz layers 237 (Fig. 21) on the inner surfaces defining the cavity 22 and the etch channels 233. The residual Si02 layers 237 can be formed by oxidation by pushing 2.25 1/m of HZ and OZ at 850°C for 10 minutes and oxidizing with 2.25 1/m of HZ and 02 at 850°C for 30 minutes. The SiOz layers 237 formed on the inner surfaces of the etch channels 233 substantially closes the etch channels 233. The etch channels 233 are further sealed by depositing sealing polysilicon which fills any openings which may remain between the SiOz layers 237. In the illustrated embodiment, the sealing polysilicon is deposited at 580°C to 650°C to a final thickness of- about 1000 angstroms. Excess amounts of the deposited sealing polysilicon thereafter are etched away, leaving 2i760~2 -2s-residual sealing polysilicon which fills and closes any openings in the SiOz layer 237. The sealing polysilicon can be etched in any suitable manner. In the illustrated embodiment, the sealing polysilicon is isotropically plasma etched with SF6. The photoresist thereafter is removed. Upon sealing the etch channels 233, OZ remaining in the cavity 22 continues to react until substantially all Ozin the cavity 22 is consumed. The cavity 22 thus is sealed and evacuated. -The cavity being evacuated minimizes dampening of the beam and provides a high Q value.
The insulating layer 234 (Fig. 21) is deposited over the cover layer 92 and the n-type epitaxial layer 208 in a suitable manner. Any suitable insulating material can be used. In the illustrated embodiment, the insulating material is silicon nitride.
In the illustrated embodiment, the silicon nitride is deposited by low pressure chemical vapor deposition (LPCVD) at 835°C to a thickness of about 950 +/- 90 angstroms. The insulating layer 234 insulates the force transducer 10 from undesired electrical contact The electrical contacts are deposited in a suitable manner for connection to the integrated circuitry 12 (Fig. 24). In the illustrated embodiment, electrical contact cavities 235 (Fig. 22) are etched for receiving the electrical contacts 236 (Fig. 24).
The electrical contact cavities 235 are patterned by applying photoresist and exposing the photoresist using 2i 76052 the electrical contact cavity mask shown in Fig. 23.
The insulating layer 234 is etched with a 50:1 buffered oxide etching solution for a period of about 2.5 minutes to form the electrical contact cavities 235 (Fig. 22). The photoresist thereafter is removed. The electrical contacts 236 (Fig. 24) are then deposited in the electrical contact cavities 235. In the illustrated embodiment, the electrical contacts 232 are aluminum. The aluminum is deposited to a thickness of about 7500 angstroms and etched using the mask shown in Fig. 25. Thereafter, the aluminum electrical contacts 232 are alloyed into contact with the silicon by alloying at 450°C with 15~ HZ and 85~ Ni.
In operation of the force transducer 10, the beam 52 is caused to resonate by operation of the integrated circuitry 12 and the capacitive drive 120.
Strain exerted on the beam 52 in the direction of the longitudinal axis changes the resonant frequency of the beam 52. The resistance of the piezoresistor 224 changes in relation to the change in the resonant frequency of the beam 52 and thus changes the output of the integrated circuitry 12. The output signal from the integrated circuitry 12 thus changes in relation to changes in the strain sensed by the beam 52.
The force transducer can be inexpensively formed by single-sided fabrication in relatively few steps. The beam is integral with the wafer and 2i7b052 _2,_ therefore provides a force transducer of high sensitivity and accuracy.
Various features and advantages of the invention are set forth in the following claims.

Claims (12)

1. A method of forming apparatus including a force transducer having a resonating silicon beam within a cavity in a silicon substrate, said method comprising the acts of:
a. providing said silicon substrate having an upper surface;
b. implanting a buried layer of a dopant, said dopant being one of the n-type and the p-type dopant, in said substrate;
c. implanting in said substrate a layer of a dopant of the other of the n-type and the p-type over said buried layer of said one of the n-type and the p-type dopant;
d. depositing an epitaxial layer on said upper surface of said substrate to completely cover said layer of dopant, said epitaxial layer including a dopant of said one of the n-type and the p-type;
e. implanting a pair of spaced sinkers through said epitaxial layer and into electrical connection with said layer of dopant, each of said sinkers including a dopant of the other of the n-type and the p-type;
f. anodizing said substrate to form porous silicon of said sinkers and said layer of dopant;
g. oxidizing said porous silicon to form silicon dioxide;
h. dissolving said silicon dioxide by etching to form said cavity and said beam supported within said cavity to resonate within said cavity, so that said cavity includes a pair of spaced side walls, a pair of spaced end walls extending between said side walls, and a bottom wall, and so that said beam extends from one of said end walls of said cavity to said other of said end walls of said cavity, and so that said beam has side surfaces spaced from said side walls of said cavity and a lower surface spaced from said bottom wall; and i. providing a capacitive drive for causing resonant motion of said beam, said capacitive drive including a first electrode below said beam, a second electrode in said beam, and a third electrode above said beam wherein said buried layer of said one of the n-type and the p-type dopant acts as said first electrode.
2. A method as set forth in claim 1 and further including before said act (f) the act of implanting a sinker of said one of the n-type and the p-type dopant through said epitaxial layer and into electrical connection with said buried layer of said one of the n-type and the p-type dopant.
3. A method as set forth in claim 1 and further including before said act (h):
forming a sacrificial layer over said epitaxial layer; and forming over said sacrificial layer a cover layer;
wherein said act (h) further includes dissolving said sacrificial layer such that said cover layer has a lower surface which defines an upper wall of said cavity, and such that said beam has an upper surface spaced from said upper wall of said cavity.
4. A method as set forth in claim 1 and further including forming a cover layer over said cavity and sealing and evacuating said cavity and providing an electronic circuit element mounted on said beam so as to generate an electrical output signal in response to said resonance.
5. A method of forming apparatus including a force transducer having a resonating silicon beam within a cavity in a silicon substrate, said method comprising the acts of:
a. providing said silicon substrate having an upper surface;
b. implanting a buried layer of a dopant, said dopant being one of the n-type and the p-type dopant, in the substrate;
c. implanting in said substrate a layer of a dopant of the other of the n-type and the p-type over said buried layer of said one of the n-type and the p-type dopant;
d. depositing an epitaxial layer on said upper surface of said substrate to completely cover said layer of dopant, said epitaxial layer including a dopant of said one of the n-type and the p-type.
e. implanting a pair of spaced sinkers through said epitaxial layer and into electrical connection with said layer of dopant, each of said sinkers including a dopant of the other of the n-type and the p-type.
f. anodizing said substrate to form porous silicon of said sinkers and said layer of dopant;
g. oxidizing said porous silicon to form silicon dioxide;
h. forming a sacrificial layer over said epitaxial layer;
i. forming over said sacrificial layer a cover layer;

j. dissolving said silicon dioxide and said sacrificial layer by etching to form said cavity and said beam supported within said cavity to resonate within said cavity, so that said cavity includes a pair of spaced side walls, a pair of spaced end walls extending between said side walls, a bottom wall, and a top wall, and so that said beam extends from one of said end walls of said cavity to said other of said end walls of said cavity, and so that said beam has side surfaces spaced from said side walls of said cavity, a lower surface spaced from said bottom wall and an upper surface spaced from said top wall;
k. providing a capacitive drive for causing resonant motion of said beam, said capacitive drive including a first electrode and wherein the buried layer of said one of the n-type and the p-type dopant acts as said first electrode of said capacitive drive.
6. A method as set forth in claim 5 further including the act of providing a capacitive drive for causing resonant motion of said beam, wherein said capacitive drive including the first electrode below said beam, a second electrode in said beam, and a third electrode above said beam.
7. A method as set forth in claim 5 and further including before said act (f) the act of implanting a sinker of said one of the n-type and the p-type dopant through said epitaxial layer and into electrical connection with said buried layer of said one of the n-type and the p-type dopant.
8. A method as set forth in claim 5 and further including forming a cover layer over said cavity and sealing and evacuating said cavity and providing an electronic circuit element mounted on said beam so as to generate an electrical output signal in response to said resonance.
9. A method of forming apparatus including a force transducer having a single crystal resonating silicon beam within a cavity in a single crystal silicon substrate, said method comprising the acts of:
a. providing said single crystal silicon substrate having an upper surface;
b. implanting a buried layer of a dopant, said dopant being one of the n-type and the p-type dopant, in said substrate;
c. implanting in said single crystal substrate a layer of a dopant of the other of the n-type and the p-type over said buried layer;
d. depositing an epitaxial layer on said upper surface of said single crystal substrate to completely cover said layer of dopant, said epitaxial layer including a dopant of said one of the n-type and the p-type;
e. implanting a pair of spaced sinkers through said epitaxial layer and into electrical connection with said layer of dopant, each of said sinkers including a dopant of the other of the n-type and the p-type;
f. anodizing said substrate to form porous silicon of said sinkers and said layer of dopant;
g. oxidizing said porous silicon to form silicon dioxide;

h. dissolving said silicon dioxide by etching to form said cavity and said single crystal silicon beam supported within said cavity to resonate within said cavity, so that said cavity includes a pair of spaced side walls, a pair of spaced end walls extending between said side walls, and a bottom wall, and so that said beam extends from one of said end walls of said cavity to said other of said end walls of said cavity, and so that said beam has side surfaces spaced from said side walls of said cavity and a lower surface spaced from said bottom wall; and i. providing a capacitive drive for causing resonant motion of said beam, said capacitive drive including a first electrode below said single crystal silicon beam, a second electrode in said beam, and a third electrode above said beam and wherein the buried layer acts as said first electrode.
10. A method as set forth in claim 9 and further including before said act (e) the act of implanting a sinker of said one of the n-type and the p-type dopant through said epitaxial layer and into electrical connection with said buried layer of said one of the n-type and the p-type dopant.
11. A method as set forth in clam 9 and further including before said act (g):
forming a sacrificial layer over said epitaxial layer; and forming over said sacrificial layer a cover layer;
wherein said act (g) further includes dissolving said sacrificial layer such that said cover layer has a lower surface which defines an upper wall of said cavity, and such that said beam has an upper surface spaced from said upper wall of said cavity.
12. A method as set forth in claim 9 and further including forming a cover layer over said cavity and sealing and evacuating said cavity and providing an electronic circuit element mounted on said beam so as to generate an electrical output signal in response to said resonance.
CA002176052A 1995-06-07 1996-05-08 Transducer having a resonating silicon beam and method for forming same Abandoned CA2176052A1 (en)

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Families Citing this family (45)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100210848B1 (en) * 1996-08-26 1999-07-15 구본준 Manufacturing method of silicon micro pattern
JP3301334B2 (en) * 1997-01-31 2002-07-15 三菱電機株式会社 Sensor element and method of manufacturing the same
DE19839606C1 (en) * 1998-08-31 2000-04-27 Siemens Ag Micromechanical component and method for its production
US6309983B1 (en) * 1999-06-03 2001-10-30 Infineon Technologies Ag Low temperature sacrificial oxide formation
US6268635B1 (en) * 1999-08-04 2001-07-31 Jds Uniphase Inc. Dielectric links for microelectromechanical systems
US7427526B2 (en) * 1999-12-20 2008-09-23 The Penn State Research Foundation Deposited thin films and their use in separation and sacrificial layer applications
AU2001261026A1 (en) * 2000-04-17 2001-10-30 The Penn State Research Foundation Deposited thin films and their use in separation and sarcrificial layer applications
US7008812B1 (en) * 2000-05-30 2006-03-07 Ic Mechanics, Inc. Manufacture of MEMS structures in sealed cavity using dry-release MEMS device encapsulation
US7153717B2 (en) * 2000-05-30 2006-12-26 Ic Mechanics Inc. Encapsulation of MEMS devices using pillar-supported caps
DE10032579B4 (en) * 2000-07-05 2020-07-02 Robert Bosch Gmbh Method for producing a semiconductor component and a semiconductor component produced by the method
US6800988B1 (en) * 2000-07-11 2004-10-05 Technion Research & Development Foundation Ltd. Voltage and light induced strains in porous crystalline materials and uses thereof
DE10036724A1 (en) * 2000-07-27 2002-02-14 Infineon Technologies Ag Production of a trench in a semiconductor substrate comprises arranging a mask on the substrate having a window, electrochemically etching the surface exposed by the window, forming a porous substrate and removing the porous substrate
DE10054484A1 (en) 2000-11-03 2002-05-08 Bosch Gmbh Robert Micromechanical component and corresponding manufacturing method
DE10114036A1 (en) * 2001-03-22 2002-10-02 Bosch Gmbh Robert Process for the production of micromechanical sensors and sensors produced therewith
US6734762B2 (en) * 2001-04-09 2004-05-11 Motorola, Inc. MEMS resonators and method for manufacturing MEMS resonators
US6800912B2 (en) * 2001-05-18 2004-10-05 Corporation For National Research Initiatives Integrated electromechanical switch and tunable capacitor and method of making the same
US6448103B1 (en) 2001-05-30 2002-09-10 Stmicroelectronics, Inc. Method for making an accurate miniature semiconductor resonator
US6878567B2 (en) * 2001-06-29 2005-04-12 Intel Corporation Method and apparatus for fabrication of passivated microfluidic structures in semiconductor substrates
US20040005258A1 (en) * 2001-12-12 2004-01-08 Fonash Stephen J. Chemical reactor templates: sacrificial layer fabrication and template use
US7309620B2 (en) * 2002-01-11 2007-12-18 The Penn State Research Foundation Use of sacrificial layers in the manufacture of high performance systems on tailored substrates
US6707351B2 (en) * 2002-03-27 2004-03-16 Motorola, Inc. Tunable MEMS resonator and method for tuning
JP2004103613A (en) * 2002-09-04 2004-04-02 Toshiba Corp Semiconductor device and its manufacturing method
JP2004228150A (en) * 2003-01-20 2004-08-12 Canon Inc Etching method
US7492019B2 (en) * 2003-03-07 2009-02-17 Ic Mechanics, Inc. Micromachined assembly with a multi-layer cap defining a cavity
US7094621B2 (en) * 2003-03-05 2006-08-22 Jbcr Innovations, L.L.P. Fabrication of diaphragms and “floating” regions of single crystal semiconductor for MEMS devices
EP1493711B1 (en) * 2003-07-04 2008-04-16 STMicroelectronics S.r.l. Process for the obtainment of a semiconductor device comprising a suspended micro-system and corresponding device
US7145213B1 (en) 2004-05-24 2006-12-05 The United States Of America As Represented By The Secretary Of The Air Force MEMS RF switch integrated process
US7381583B1 (en) 2004-05-24 2008-06-03 The United States Of America As Represented By The Secretary Of The Air Force MEMS RF switch integrated process
US7231829B2 (en) * 2005-03-31 2007-06-19 Medtronic, Inc. Monolithic integrated circuit/pressure sensor on pacing lead
US9616223B2 (en) 2005-12-30 2017-04-11 Medtronic, Inc. Media-exposed interconnects for transducers
DE102006004209B3 (en) * 2006-01-30 2007-09-06 Infineon Technologies Ag Micromechanical component and method for producing a micromechanical component
US7442599B2 (en) * 2006-09-15 2008-10-28 Sharp Laboratories Of America, Inc. Silicon/germanium superlattice thermal sensor
EP2104948A2 (en) 2007-02-20 2009-09-30 Qualcomm Mems Technologies, Inc. Equipment and methods for etching of mems
CN101652317B (en) 2007-04-04 2012-12-12 高通Mems科技公司 Eliminate release etch attack by interface modification in sacrificial layers
US7719752B2 (en) 2007-05-11 2010-05-18 Qualcomm Mems Technologies, Inc. MEMS structures, methods of fabricating MEMS components on separate substrates and assembly of same
EP2181355A1 (en) 2007-07-25 2010-05-05 Qualcomm Mems Technologies, Inc. Mems display devices and methods of fabricating the same
US8023191B2 (en) 2008-05-07 2011-09-20 Qualcomm Mems Technologies, Inc. Printable static interferometric images
JP5427392B2 (en) * 2008-10-22 2014-02-26 株式会社デジアイズ Load sensor, scale
US8353215B2 (en) * 2009-07-13 2013-01-15 Delatorre Leroy C Torque output differential pressure sensor
EP2365521B1 (en) * 2010-01-22 2018-12-26 IMEC vzw Thin film wafer level package
DE102010029302B4 (en) 2010-05-26 2021-08-19 Robert Bosch Gmbh Process for the production of a wide variety of thin chips
US9105751B2 (en) 2011-11-11 2015-08-11 International Business Machines Corporation Integrated semiconductor devices with single crystalline beam, methods of manufacture and design structure
US8629036B2 (en) 2011-11-11 2014-01-14 International Business Machines Corporation Integrated semiconductor devices with amorphous silicon beam, methods of manufacture and design structure
US8546240B2 (en) 2011-11-11 2013-10-01 International Business Machines Corporation Methods of manufacturing integrated semiconductor devices with single crystalline beam
US11352169B2 (en) 2019-01-18 2022-06-07 Rehrig Pacific Company Pallet assembly

Family Cites Families (41)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4822673B1 (en) * 1969-11-13 1973-07-07
US3909924A (en) * 1974-03-27 1975-10-07 Nat Semiconductor Corp Method of fabrication of silicon pressure transducer sensor units
GB1601547A (en) * 1977-05-30 1981-10-28 Yokogawa Electric Works Ltd Force detector
GB2121953B (en) * 1982-06-10 1985-09-04 Itt Ind Ltd Improvements in transducers
JPS60111129A (en) * 1983-11-21 1985-06-17 Yokogawa Hokushin Electric Corp Pressure sensor
US4532700A (en) * 1984-04-27 1985-08-06 International Business Machines Corporation Method of manufacturing semiconductor structures having an oxidized porous silicon isolation layer
US4628591A (en) * 1984-10-31 1986-12-16 Texas Instruments Incorporated Method for obtaining full oxide isolation of epitaxial islands in silicon utilizing selective oxidation of porous silicon
US4665610A (en) * 1985-04-22 1987-05-19 Stanford University Method of making a semiconductor transducer having multiple level diaphragm structure
US4744863A (en) * 1985-04-26 1988-05-17 Wisconsin Alumni Research Foundation Sealed cavity semiconductor pressure transducers and method of producing the same
US4853669A (en) * 1985-04-26 1989-08-01 Wisconsin Alumni Research Foundation Sealed cavity semiconductor pressure transducers and method of producing the same
JPS6263828A (en) * 1985-09-06 1987-03-20 Yokogawa Electric Corp Vibration type transducer and its manufacture
US4766666A (en) * 1985-09-30 1988-08-30 Kabushiki Kaisha Toyota Chuo Kenkyusho Semiconductor pressure sensor and method of manufacturing the same
US4771638A (en) * 1985-09-30 1988-09-20 Kabushiki Kaisha Toyota Chuo Kenkyusho Semiconductor pressure sensor
GB8530809D0 (en) * 1985-12-13 1986-01-22 Gen Electric Co Plc Sensor
JPS6381867A (en) * 1986-09-25 1988-04-12 Yokogawa Electric Corp Semiconductor diffusion strain gauge
US4975390A (en) * 1986-12-18 1990-12-04 Nippondenso Co. Ltd. Method of fabricating a semiconductor pressure sensor
US4805456A (en) * 1987-05-19 1989-02-21 Massachusetts Institute Of Technology Resonant accelerometer
JPH0797643B2 (en) * 1987-07-08 1995-10-18 日産自動車株式会社 Method for manufacturing pressure transducer
JP2701845B2 (en) * 1987-08-21 1998-01-21 株式会社東海理化電機製作所 Manufacturing method of silicon thin film
US4800759A (en) * 1987-08-31 1989-01-31 Yokogawa Electric Corporation Semiconductor pressure converter
US4771639A (en) * 1987-09-02 1988-09-20 Yokogawa Electric Corporation Semiconductor pressure sensor
JPH01136378A (en) * 1987-11-24 1989-05-29 Nissan Motor Co Ltd Manufacture of pressure transducer
US4897360A (en) * 1987-12-09 1990-01-30 Wisconsin Alumni Research Foundation Polysilicon thin film process
KR920007501B1 (en) * 1988-02-04 1992-09-04 요꼬가와덴기 가부시기가이샤 Signal conditioners
US4784721A (en) * 1988-02-22 1988-11-15 Honeywell Inc. Integrated thin-film diaphragm; backside etch
JPH07104217B2 (en) * 1988-05-27 1995-11-13 横河電機株式会社 Vibration transducer and manufacturing method thereof
US5110373A (en) * 1988-09-13 1992-05-05 Nanostructures, Inc. Silicon membrane with controlled stress
US5009108A (en) * 1988-09-16 1991-04-23 Yokogawa Electric Corporation Vibrating type transducer
US4901570A (en) * 1988-11-21 1990-02-20 General Motors Corporation Resonant-bridge two axis microaccelerometer
US4893509A (en) * 1988-12-27 1990-01-16 General Motors Corporation Method and product for fabricating a resonant-bridge microaccelerometer
US5095401A (en) * 1989-01-13 1992-03-10 Kopin Corporation SOI diaphragm sensor
US4945769A (en) * 1989-03-06 1990-08-07 Delco Electronics Corporation Semiconductive structure useful as a pressure sensor
US4993143A (en) * 1989-03-06 1991-02-19 Delco Electronics Corporation Method of making a semiconductive structure useful as a pressure sensor
US4889590A (en) * 1989-04-27 1989-12-26 Motorola Inc. Semiconductor pressure sensor means and method
JP2811768B2 (en) * 1989-07-17 1998-10-15 株式会社デンソー Semiconductor type acceleration sensor and method of manufacturing the same
US5090254A (en) * 1990-04-11 1992-02-25 Wisconsin Alumni Research Foundation Polysilicon resonating beam transducers
CN1018844B (en) * 1990-06-02 1992-10-28 中国科学院兰州化学物理研究所 Antirust dry film lubricant
CN1027011C (en) * 1990-07-12 1994-12-14 涂相征 Silicon-piezoelectric acceleration sensor and manufacture thereof
JPH0590615A (en) * 1991-09-30 1993-04-09 Yokogawa Electric Corp Manufacture of vibrating-type transducer
US5332469A (en) * 1992-11-12 1994-07-26 Ford Motor Company Capacitive surface micromachined differential pressure sensor
US5427975A (en) * 1993-05-10 1995-06-27 Delco Electronics Corporation Method of micromachining an integrated sensor on the surface of a silicon wafer

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JPH098330A (en) 1997-01-10
DE69601977T2 (en) 1999-12-02
US6118164A (en) 2000-09-12
EP0747684A1 (en) 1996-12-11
DE69601977D1 (en) 1999-05-12
EP0747684B1 (en) 1999-04-07
US5834333A (en) 1998-11-10

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